| contributor author | N. L. Sanger | |
| contributor author | R. P. Shreeve | |
| date accessioned | 2017-05-08T23:23:42Z | |
| date available | 2017-05-08T23:23:42Z | |
| date copyright | July, 1986 | |
| date issued | 1986 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28577#42_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/101852 | |
| description abstract | The midspan section of a previously reported controlled-diffusion compressor stator has been experimentally evaluated in cascade. Measurements were taken over a range of incidence angles for blade chord Reynolds numbers from 470,000 to 690,000. Blade chord length was 12.7 cm, aspect ratio was 2.0, and solidity was 1.67. Measurements included conventional cascade performance parameters as well as blade surface pressures. Computations were made for the inviscid flow field, surface boundary layers, and loss for several of the blade inlet angle conditions, and compared against corresponding data. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Comparison of Calculated and Experimental Cascade Performance for Controlled-Diffusion Compressor Stator Blading | |
| type | Journal Paper | |
| journal volume | 108 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.3262023 | |
| journal fristpage | 42 | |
| journal lastpage | 50 | |
| identifier eissn | 1528-8900 | |
| keywords | Diffusion (Physics) | |
| keywords | Compressors | |
| keywords | Cascades (Fluid dynamics) | |
| keywords | Stators | |
| keywords | Blades | |
| keywords | Chords (Trusses) | |
| keywords | Measurement | |
| keywords | Reynolds number | |
| keywords | Boundary layers | |
| keywords | Computation AND Inviscid flow | |
| tree | Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001 | |
| contenttype | Fulltext | |
